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%  NOTE 
% % % %  If it is not possible to start the engine: -adopt glide configuration as in 3.4 - GLIDING -carry out emergency landing in accordance with 3.5.1 - EMERGENCY LANDING WITH ENGINE OFF 
% 
%  10.  AVIONIC MASTER .................... ON, if required 

Doc. No. 6.01.05-E  Revision 1  03-Mar-2003  Page 3 - 11 

3.2.5 RESTARTING THE ENGINE WITH STATIONARY PROPELLER
NOTE
Restarting the engine with stationary propeller is possible at altitudes below 6500 ft pressure altitude.
1.  
Airspeed for best glide angle ............ 73 KIAS (1150 kg, 2535 lb) 68 KIAS (1000 kg, 2205 lb) 60 KIAS (850 kg, 1874 lb)

2.
ENGINE MASTER ....................  OFF

3.
Power lever .........................  MAX

4.
Emergency fuel valve..................  check NORMAL

5.
Alternate air .........................  OPEN

6.
Fuel transfer pump ....................  ON

7.
AVIONIC MASTER....................  OFF

8.
ELECTRIC MASTER ..................  ON

9.
ENGINE MASTER ....................  ON

NOTE
Only if the ENGINE MASTER is switched OFF and ON again, glowing will be initiated. Glowing must be initiated shortly before the restart attempt. If glowing was done above 6500 ft pressure altitude, it must be repeated.
10.  ELECTRIC MASTER .................. START (release when engine is running)
Doc. No. 6.01.05-E  Revision 1  03-Mar-2003  Page 3 - 12 

NOTE
By increasing the airspeed above approximately 105 KIAS, the propeller will begin to rotate due to windmilling and the engine can thus be started. For this, the ELECTRIC MASTER should be set to ON (see 3.2.4 RESTARTING THE ENGINE WITH WINDMILLING PROPELLER). A loss of altitude of at least 1000 ft (300 meters) must be expected.
If it is not possible to start the engine:
-adopt glide configuration as in 3.4 - GLIDING -carry out emergency landing as in 3.5.1 - EMERGENCY
LANDING WITH ENGINE OFF
CAUTION
Engine restart following an engine fire should only be attempted if it is unlikely that a safe emergency landing can be made. It must be expected that engine restart is impossible after an engine fire.
Doc. No. 6.01.05-E  Revision 1  03-Mar-2003  Page 3 - 13 

3.2.6 DEFECTIVE RPM REGULATING SYSTEM
CAUTION
Following a failure of the governor the RPM should be adjusted with the power lever. Every effort should be made not to exceed 2500 RPM.
CAUTION
The power lever should be moved slowly, in order to avoid over-speeding and excessively rapid RPM changes. The light wooden propeller blades produce more rapid RPM changes than metal blades.
　
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